EP2143960A1 - Dispositif pour maintenir un système de palier - Google Patents

Dispositif pour maintenir un système de palier Download PDF

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Publication number
EP2143960A1
EP2143960A1 EP09008722A EP09008722A EP2143960A1 EP 2143960 A1 EP2143960 A1 EP 2143960A1 EP 09008722 A EP09008722 A EP 09008722A EP 09008722 A EP09008722 A EP 09008722A EP 2143960 A1 EP2143960 A1 EP 2143960A1
Authority
EP
European Patent Office
Prior art keywords
bearing
holding
bearing shell
hollow shaft
hollow axle
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP09008722A
Other languages
German (de)
English (en)
Other versions
EP2143960B1 (fr
Inventor
Peter Weimer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus DS GmbH
Original Assignee
Astrium GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Astrium GmbH filed Critical Astrium GmbH
Publication of EP2143960A1 publication Critical patent/EP2143960A1/fr
Application granted granted Critical
Publication of EP2143960B1 publication Critical patent/EP2143960B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
    • G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
    • G02B7/182—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
    • G02B7/1821—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors for rotating or oscillating mirrors
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B23/00—Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices
    • G02B23/16—Housings; Caps; Mountings; Supports, e.g. with counterweight

Definitions

  • the invention relates to a device for, in particular temporary, force-free mounting of a bearing system with a rotation axis.
  • Flexpivot bearings For pivotal movements in an angular range of about +/- 25 °, so-called.
  • Flexpivot bearings have been established, which follow their axis of rotation very precisely by an elastic deformation of integrated flat spring elements.
  • Flexpivot bearings also have the advantage that no friction occurs between the rotating parts of the bearing system.
  • flexpivot bearings are very sensitive to lateral and axial forces under optimum weighting under weightlessness. Such forces usually occur when launching a rocket, with which the scanning system is moved into orbit.
  • HDRM hold down and release mechanisms
  • a device for, in particular temporary, force-free mounting of a bearing system with a rotation axis comprises a cylindrical hollow axle for concentrically receiving and holding the bearing system.
  • the center or symmetry axis of the cylindrical hollow axle coincides with the axis of rotation of the bearing system when it is received and supported by the cylindrical hollow axle.
  • the device further comprises a bearing shell which can be fastened to the hollow axle by means of a holding and releasing device in such a manner that all lateral and axial forces acting on the device can be guided via the cylindrical hollow axle in axle receptacles without a load being applied to the bearing system.
  • the arrangement of the storage system in the cylindrical hollow axle, which is connected to a controlled by the holding and releasing device bearing shell, allows the provision of a device which has no over-determination of the storage system.
  • the device can be realized with minimal assembly weight with compact dimensions.
  • the device according to the invention makes it possible to dimension the bearing system as little as possible, since this only needs to be designed for orbital loads and thus can only build up low torques.
  • Another advantage of the invention is that it can be used or used multiple times.
  • the bearing axis surrounds the hollow axis in the circumferential direction, so that a uniform absorption of the lateral and axial forces on the cylindrical hollow shaft is ensured.
  • the hollow axle is expediently formed from two, in particular symmetrically arranged, partial axes, which are connected to one another via the bearing system.
  • the applied to the device lateral and axial forces are passed over the two sub-axes in Achsfactn, the storage system is decoupled from these forces, as long as the holding and releasing device is locked.
  • each of the sub-axes in one embodiment at their ends facing each other on a flange with a bore. It is intended to connect the storage system with the flanges of the sub-axes.
  • the connection of the storage system with the hollow axle or with the two partial axes is advantageously carried out by a material connection.
  • the material connection with the aid of an electric plasma welding system can be made later and along the entire circumference of the storage system.
  • the sub-axes at their ends facing each other on its outer side in each case a groove into which the bearing shell engages positively.
  • the groove in this case runs in particular along an outer circumference of the partial axis.
  • the respective grooves are continuous, i. circumferential, trained.
  • the bearing shell comprises in particular a first and a second bearing shell part, which are rotatably connected to one another at their first end and which are connected to each other at its second opposite end with the holding and releasing device with high bias.
  • the connection of the two bearing shell parts at their first end and their fixation by applying a high bias by means of the holding and releasing device allows a structurally simple construction and the reliable provision of a non-determined holding mechanism for the storage system.
  • the high bias at the second ends allows for automatic "opening" of the bearing cup as soon as the holding and releasing device no longer applies a force for compressing the second ends.
  • a spring element is additionally provided between the second ends of the bearing shell parts, which causes the defined opening of the bearing shell parts upon actuation of the holding and releasing device for unlocking the device according to the invention.
  • the holding and releasing device comprises a bolt-separating mechanism.
  • This can be formed, for example, in the form of a known Frangibolt mechanism which, with appropriate control, solves the mechanical connection of the second ends of the bearing shell parts and thus terminates the action of force on the hollow axis.
  • the hollow axle is formed, in particular, from a highly rigid material, such as titanium. As already explained, this makes it possible to dimension the storage system only on orbital loads, which thus build up only low torques, as is required for high-precision scanning elements.
  • the bearing shell is made of the same high-strength material (titanium).
  • the hollow shaft is made in one clamping.
  • a tension-free Flexpivot bearing is used, which comply with an elastic deformation of integrated flat spring elements their axis of rotation very accurately, without causing a friction between the rotating parts.
  • Such Flexpivot bearings are known from the prior art.
  • a device In order to protect a bearing system 1 designed as a flex pivot bearing against lateral and axial forces, such as during a rocket launch, a device according to the invention comprises a hollow axle 3 formed from two partial axles 3a, 3b.
  • the hollow axle 3 forms a bearing axle.
  • the sub-axes 3a, 3b are, as out Fig. 1 shows symmetrically arranged to each other and in one Manufacturing made.
  • the hollow axle 3 or its sub-axles 3a, 3b are preferably formed from a highly rigid material (eg titanium).
  • the sub-axles 3 a, 3 b have a flange 6 a, 6 b with a bore for receiving and holding the flexpivot bearing 1.
  • the Flexpivot bearing 1 is inserted into the bores of the flanges 6a, 6b and, for example, welded on both sides and around with the aid of an electric plasma welding system.
  • the flex pivot bearing 1 comes to lie in such a way in the hollow shaft 3, that an axis of rotation of the flexpivot bearing comes to rest with an axis of symmetry of the hollow shaft 3. Furthermore, the arrangement takes place in such a way that, when the device is unlocked, a rotation of the two mutually prestressed sections of the flexpivot bearing 1 is possible.
  • a bearing shell 2 surrounding the hollow shaft 3 is provided.
  • the bearing shell 2 comprises two bearing shell parts 2a, 2b, which at a first end 8a, 8b (see. FIG. 3 ) are rotatably connected to each other via a hinge 18.
  • a high-strength material is preferably used, such as titanium.
  • a first end 8a, 8b opposite the second end 9a, 9b of the bearing shell parts 2a, 2b designed as Bolzentrennmechanismus holding and releasing device 4 is provided. In the exemplary embodiment, this is a so-called. Frangibolt mechanism.
  • each of the hollow shafts 3a, 3b has in the region of the flexpivot bearing 1 a groove 7a or 7b, which extend along the circumference of the respective sub-axes 3a, 3b.
  • the bearing shell 2 is arranged on the hollow axle 3 in such a way that the webs forming the groove 10a, 10b project in a form-fitting manner into the grooves 7a or 7b of the part axles 3a, 3b. in this connection
  • the mutually adjacent webs of the grooves 7a and 7b protrude or border on the bottom of the grooves 10a, 10b of the bearing shell parts 2a, 2b.
  • the second ends 9a, 9b of the bearing shell parts 2a, 2b are connected to each other via the Frangibolt mechanism 4 with high bias. Between the second ends 9a, 9b, a spring element 5 is arranged, which in an activation of the Frangibolt mechanism 4, an opening of the bearing shell parts 2a, 2b supports (see. FIG. 2 such as FIG. 5 ).
  • the design of the known Frangibolt mechanism 4 can best the Figures 2 and 5 be removed.
  • the Frangibolt mechanism is a bolt-centering mechanism. For this purpose, this has a bolt 12 with a groove 13 in the interior of a jacket 14. At a first end, the bolt 12 has a bolt head 19, which is supported on the jacket 14. At its opposite end, the bolt 12 is screwed to a nut 16. Between the nut 16 and the second end 9b of the bearing shell part 2b, an intermediate element 17 is arranged for receiving power. By screwing a high bias on the bearing shell parts 2a, 2b can be exercised.
  • an actuator not shown in the figures, which is provided in the interior of the shell 14 and adjacent to the surface of the bolt 12, a breaking of the bolt at a predefined position, usually in the region of the groove 13, can be effected. Due to the high bias and with the support of the spring element 5, the already described opening of the bearing shell 2 takes place to release the Flexpivot bearing.
  • the actuator can be formed for example by a heating element, which can be heated via connecting lines 15.
  • the connecting lines 15 for driving the actuator can, for example, the Figures 3 and 5 be removed.
  • the device according to the invention comprising the hollow axle, the bearing shell and the holding and releasing device, has no over-determination to the Flexpivot bearing arranged in the interior of the hollow axle.
  • the Flexpivot bearing can be dimensioned as small as possible, since this only needs to be dimensioned for orbital loads and thus has only low reaction torques. It is expedient for the hollow axle, a highly rigid material such. As titanium, to use.
  • the device according to the invention then has a small size with the minimum assembly weight.
  • qualified bolt-driving mechanisms may be used, e.g. the explained Frangibolt mechanism.
  • the activation bolt need not, as usually required, completely pulled and collected, since a small activation path (opening distance) in the range of 0.5 to 1.0 mm is sufficient.
  • the device according to the invention can be used or used several times.
  • the device may also be implemented as a so-called "low shock" mechanism, for example by bracing the bearing shell parts with the aid of a heavily geared geared motor.
EP09008722.2A 2008-07-08 2009-07-03 Dispositif pour maintenir un système de palier Active EP2143960B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102008031910A DE102008031910B4 (de) 2008-07-08 2008-07-08 Vorrichtung zur Halterung eines Lagersystems

Publications (2)

Publication Number Publication Date
EP2143960A1 true EP2143960A1 (fr) 2010-01-13
EP2143960B1 EP2143960B1 (fr) 2014-06-18

Family

ID=41058525

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09008722.2A Active EP2143960B1 (fr) 2008-07-08 2009-07-03 Dispositif pour maintenir un système de palier

Country Status (4)

Country Link
US (1) US8333514B2 (fr)
EP (1) EP2143960B1 (fr)
DE (1) DE102008031910B4 (fr)
ES (1) ES2500566T3 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104360455B (zh) * 2014-10-16 2016-08-24 中国科学院上海技术物理研究所 一种空间遥感相机反射镜柔性虎克铰支撑机构

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Publication number Priority date Publication date Assignee Title
US9259812B1 (en) * 2013-06-26 2016-02-16 The Boeing Company Clamp assembly and method
US20150267855A1 (en) * 2014-03-21 2015-09-24 The Ford Meter Box Company, Inc. Installation aid for water pipeline repair clamp
US10119631B2 (en) * 2016-02-05 2018-11-06 Hellermanntyton Corporation Adjustable p-clamp
US10903632B2 (en) 2016-02-05 2021-01-26 Hellermanntyton Corporation Adjustable P-clamp with multiple mounting options
US10518907B2 (en) * 2016-09-13 2019-12-31 Ensign-Bickford Aerospace & Defense Company Spacecraft device initiation system
US10549869B2 (en) 2016-09-13 2020-02-04 Ensign-Bickford Aerospace & Defense Company Multipoint payload release system
WO2018112637A1 (fr) * 2016-12-21 2018-06-28 Macdonald, Dettwiler And Associates Inc. Mécanisme de retenue et de libération sans choc réenclenchable actionné (ares hdrm)
US10794654B2 (en) * 2018-05-01 2020-10-06 Thomas Burton Universal pintle mount for a weapon

Citations (10)

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Publication number Priority date Publication date Assignee Title
FR1338285A (fr) * 1962-11-13 1963-09-20 Double collier, de préférence pour échafaudage tubulaire
DE1286831B (de) * 1965-08-20 1969-01-09 Schnorr Adolf Kg Elastische Kupplung fuer grosse Schwenkwinkel
DE2703772A1 (de) * 1977-01-29 1978-08-03 Huennebeck Gmbh Rohrgerueststuetze aus zwei aufeinanderstehenden rohren
US4997123A (en) * 1990-05-31 1991-03-05 Lucas Aerospace Power Transmission Corp. Multi-piece flexural pivot
DE3931275A1 (de) * 1989-09-20 1991-03-28 Total Feuerschutz Gmbh Rohrkupplung
DE19812223A1 (de) * 1998-03-19 1999-09-23 Mayr Christian Gmbh & Co Kg Drehsteife, spielfreie, elastische Metallbalgkupplung zur drehmomentübertragenden Verbindung zweier Wellen
WO2003011678A1 (fr) * 2001-07-27 2003-02-13 Audi Ag Dispositif de protection durant le transport
DE10325441A1 (de) * 2003-06-05 2005-01-13 Manfred Wantoch Rohrkupplung mit Schnellverschlußsystem zur flexiblen und zugfesten Verbindung von Rohren mit und ohne Rohrendenbearbeitung
DE10346053B3 (de) * 2003-10-04 2005-04-07 Benteler Automobiltechnik Gmbh Gelenkwelle
DE102007004335A1 (de) * 2006-03-02 2007-09-06 Sem Schneider Elementebau Gmbh & Co. Kg Vorrichtung zum Verbinden von Rohrleitungsabschnitten untereinander

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US1739803A (en) * 1927-04-26 1929-12-17 Kimball Krogh Pump Company Line-shaft-bearing-lubricating device
DE2440717C2 (de) 1974-08-24 1984-05-24 INA Wälzlager Schaeffler KG, 8522 Herzogenaurach Transport- und Montagevorrichtung für Kränze von dicht beieinanderliegenden zylindrischen Wälzkörpern
US4815585A (en) * 1988-02-23 1989-03-28 Custom Metalcraft, Inc. Sanitary hanger bearing assembly
US5682069A (en) * 1994-08-30 1997-10-28 Harris Corporation Concentrically mounted vibration attenuator and method
US5906523A (en) * 1997-08-14 1999-05-25 Thordon Bearings Inc. Intermediate marine bearing with itegrated alignment system
US6413144B1 (en) 2000-12-04 2002-07-02 Colin Williams Hand-held toy for lighting when spun
CH696981A5 (de) * 2003-02-03 2008-02-29 Aquametro Ag Plombiereinrichtung an einem Durchflusszähler für Fluide.
US7857517B1 (en) * 2009-06-12 2010-12-28 Vicars Berton L Connecting rod bearing housing

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1338285A (fr) * 1962-11-13 1963-09-20 Double collier, de préférence pour échafaudage tubulaire
DE1286831B (de) * 1965-08-20 1969-01-09 Schnorr Adolf Kg Elastische Kupplung fuer grosse Schwenkwinkel
DE2703772A1 (de) * 1977-01-29 1978-08-03 Huennebeck Gmbh Rohrgerueststuetze aus zwei aufeinanderstehenden rohren
DE3931275A1 (de) * 1989-09-20 1991-03-28 Total Feuerschutz Gmbh Rohrkupplung
US4997123A (en) * 1990-05-31 1991-03-05 Lucas Aerospace Power Transmission Corp. Multi-piece flexural pivot
DE19812223A1 (de) * 1998-03-19 1999-09-23 Mayr Christian Gmbh & Co Kg Drehsteife, spielfreie, elastische Metallbalgkupplung zur drehmomentübertragenden Verbindung zweier Wellen
WO2003011678A1 (fr) * 2001-07-27 2003-02-13 Audi Ag Dispositif de protection durant le transport
DE10325441A1 (de) * 2003-06-05 2005-01-13 Manfred Wantoch Rohrkupplung mit Schnellverschlußsystem zur flexiblen und zugfesten Verbindung von Rohren mit und ohne Rohrendenbearbeitung
DE10346053B3 (de) * 2003-10-04 2005-04-07 Benteler Automobiltechnik Gmbh Gelenkwelle
DE102007004335A1 (de) * 2006-03-02 2007-09-06 Sem Schneider Elementebau Gmbh & Co. Kg Vorrichtung zum Verbinden von Rohrleitungsabschnitten untereinander

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104360455B (zh) * 2014-10-16 2016-08-24 中国科学院上海技术物理研究所 一种空间遥感相机反射镜柔性虎克铰支撑机构

Also Published As

Publication number Publication date
US20100008611A1 (en) 2010-01-14
DE102008031910B4 (de) 2010-12-02
EP2143960B1 (fr) 2014-06-18
US8333514B2 (en) 2012-12-18
DE102008031910A1 (de) 2010-01-14
ES2500566T3 (es) 2014-09-30

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